EN 2563:1997
Current
The latest, up-to-date edition.
Aerospace series - Carbone fibre reinforced plastics - Unidirectional laminates - Determination of the apparent interlaminar shear strength
22-01-1997
Foreword
1 Scope
2 Normative references
3 Definitions
4 Principle
5 Apparatus
6 Specimens
7 Procedure
8 Expression of results
9 Test report
This standard specifies the method for the determination of the apparent interlaminar shear strength of carbon fibre reinforced plastics in the form of unidirectional laminates by means of a flexural test. It is intended for specimens in which the length is parallel to the fibre direction.
| Committee |
ASD-STAN
|
| DevelopmentNote |
Supersedes PREN 2563. (11/2003)
|
| DocumentType |
Standard
|
| PublisherName |
Comite Europeen de Normalisation
|
| Status |
Current
|
| Supersedes |
| Standards | Relationship |
| NF EN 2563 : 1997 | Identical |
| NS EN 2563 : 1ED 1997 | Identical |
| PN EN 2563 : 2000 | Identical |
| SNV DIN EN 2563 : 1997 | Identical |
| NEN EN 2563 : 1997 | Identical |
| UNI EN 2563 : 1997 | Identical |
| I.S. EN 2563:1997 | Identical |
| NBN EN 2563 : 1997 | Identical |
| DIN EN 2563:1997-03 | Identical |
| UNE-EN 2563:1997 | Identical |
| BS EN 2563:1997 | Identical |
| 12/30234431 DC : 0 | BS ISO 9940 - AEROSPACE - FIRE RESISTANT HYDRAULIC FLUIDS |
| BS ISO 9940:2015 | Aerospace series. Fluid, hydraulic, phosphate ester-base, fire resistant. Technical specification |
| 14/30302298 DC : 0 | BS ISO 9940 - AEROSPACE SERIES - FLUID, HYDRAULIC, PHOSPHATE ESTER-BASE, FIRE RESISTANT - TECHNICAL SPECIFICATION |
| ISO 9940:2015 | Aerospace series Fluid, hydraulic, phosphate ester-base, fire resistant Technical specification |
| 13/30290460 DC : 0 | BS ISO 9940 - AEROSPACE SERIES - FLUID, HYDRAULIC, PHOSPHATE ESTER-BASE, FIRE RESISTANT - TECHNICAL SPECIFICATION |
| SAE AMS 3970/6 : 2011 | CARBON FIBER FABRIC REPAIR PREPREG, 120 DEGREES C (250 DEGREES F) VACUUM CURING - PART 6 - MATERIAL SPECIFICATION: CARBON FIBER FABRIC REINFORCED EPOXY PREPREG FOR REPAIR, PLAIN WEAVE FABRIC, 193 G/M[2], ADHESIVE FILM FOR REPAIR AND NON-STRUCTURAL GLASS FIBER FABRIC REINFORCED EPOXY PREPREG, 105 G/M[2] |
| SAE AMS 2980/1 : 2014 | CARBON FIBER FABRIC AND EPOXY RESIN WET LAY-UP REPAIR MATERIAL - PART 1 - GENERAL REQUIREMENTS |
| SAE AMS 3970/1 : 2011 | CARBON FIBER FABRIC REPAIR PREPREG, 120 DEGREES C (250 DEGREES F) VACUUM CURING - PART 1 - GENERAL REQUIREMENTS |
| EN 2489:1995 | Aerospace series - Fibre reinforced plastics - Determination of the action of test fluids |
| PREN 2743 : 200P1 | AEROSPACE SERIES - REINFORCED PLASTICS - STANDARD PROCEDURES FOR CONDITIONING PRIOR TO TESTING |
| PREN 2565 : 200P2 | AEROSPACE SERIES - PREPARATION OF CARBON FIBRE REINFORCED RESIN PANELS FOR TEST PURPOSES |
| PREN 2823 : 200P2 | AEROSPACE SERIES - FIBRE REINFORCED PLASTICS - DETERMINATION OF THE EFFECT OF EXPOSURE TO HUMID ATMOSPHERE ON PHYSICAL AND MECHANICAL CHARACTERISTICS |
| EN 2744:1992 | Aerospace series - Non metallic materials - Preferred test temperatures |
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